Related Books

Estimation of the Damping in Roll of Wings Through the Normal Flight Range of Lift Coefficient
Language: en
Pages: 40

Estimation of the Damping in Roll of Wings Through the Normal Flight Range of Lift Coefficient

Authors: Alex Goodman
Categories: Aerofoils
Type: BOOK - Published: 1949 - Publisher:

DOWNLOAD EBOOK

The development of three methods for calculating the damping in roll through the normal flight range of lift coefficient for wing plan forms having various swee
Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 1076

Technical Note - National Advisory Committee for Aeronautics

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1958 - Publisher:

DOWNLOAD EBOOK

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces
Language: en
Pages: 340

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces

Authors: Arthur Earl Bryson
Categories: Aeronautics
Type: BOOK - Published: 1952 - Publisher:

DOWNLOAD EBOOK

Elevated-temperature Properties of Several Titanium Carbide Base Ceramals
Language: en
Pages: 694

Elevated-temperature Properties of Several Titanium Carbide Base Ceramals

Authors: George C. Deutsch
Categories: Carbides
Type: BOOK - Published: 1949 - Publisher:

DOWNLOAD EBOOK

On a strength-to-weight ratio basis, ceramals appeared promising as gas-turbine-blade materials in the temperature range of 1600 to 2400 degrees F.
Report
Language: en
Pages: 32

Report

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1954 - Publisher:

DOWNLOAD EBOOK